GB201118553D0 - Aircraft protection device - Google Patents
Aircraft protection deviceInfo
- Publication number
- GB201118553D0 GB201118553D0 GB201118553A GB201118553A GB201118553D0 GB 201118553 D0 GB201118553 D0 GB 201118553D0 GB 201118553 A GB201118553 A GB 201118553A GB 201118553 A GB201118553 A GB 201118553A GB 201118553 D0 GB201118553 D0 GB 201118553D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- protection device
- aircraft protection
- aircraft
- protection
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB201118553A GB201118553D0 (en) | 2011-10-27 | 2011-10-27 | Aircraft protection device |
EP12187065.3A EP2586710A1 (en) | 2011-10-27 | 2012-10-03 | Aircraft protection device |
CN2012104145142A CN103085966A (en) | 2011-10-27 | 2012-10-26 | Aircraft protection device |
US13/661,454 US9017511B2 (en) | 2011-10-27 | 2012-10-26 | Aircraft protection device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB201118553A GB201118553D0 (en) | 2011-10-27 | 2011-10-27 | Aircraft protection device |
Publications (1)
Publication Number | Publication Date |
---|---|
GB201118553D0 true GB201118553D0 (en) | 2011-12-07 |
Family
ID=45373495
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB201118553A Ceased GB201118553D0 (en) | 2011-10-27 | 2011-10-27 | Aircraft protection device |
Country Status (4)
Country | Link |
---|---|
US (1) | US9017511B2 (en) |
EP (1) | EP2586710A1 (en) |
CN (1) | CN103085966A (en) |
GB (1) | GB201118553D0 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0715303D0 (en) * | 2007-08-08 | 2007-09-19 | Airbus Uk Ltd | Composite laminate structure |
EP3575071A1 (en) * | 2018-05-30 | 2019-12-04 | Crompton Technology Group Limited | Composite components |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4606516A (en) * | 1984-05-10 | 1986-08-19 | Willison George R | Aircraft protective device |
DE4313592C2 (en) * | 1993-04-26 | 2000-02-17 | Daimler Chrysler Aerospace | Wide-body aircraft |
DE19700091A1 (en) * | 1997-01-03 | 1998-07-16 | Fehrer Gummihaar | Energy absorbing panel |
US6277463B1 (en) * | 1998-08-28 | 2001-08-21 | Mcdonnell Douglas Corporation | Composite member having increased resistance to delamination and method of making same |
US6401258B1 (en) * | 1999-11-04 | 2002-06-11 | Corey Wilson | Headgear for sports fans |
US20020006523A1 (en) * | 2000-07-07 | 2002-01-17 | Obeshaw Dale Francis | Structural members containing vibration damping mechanisms and methods for making the same |
FR2869871B1 (en) * | 2004-05-04 | 2007-08-10 | Airbus France Sas | PROTECTIVE DEVICE AND REVELATION OF SHOCK FOR EDGE OF COMPOSITE STRUCTURE WITH OVERLAPPED PLATES |
GB0611804D0 (en) | 2006-06-14 | 2006-07-26 | Airbus Uk Ltd | Improved aircraft component |
GB0611802D0 (en) | 2006-06-14 | 2006-07-26 | Airbus Uk Ltd | Improved composite aircraft component |
US7618698B2 (en) * | 2007-04-06 | 2009-11-17 | The Boeing Company | Damage protection device for aircraft structure |
-
2011
- 2011-10-27 GB GB201118553A patent/GB201118553D0/en not_active Ceased
-
2012
- 2012-10-03 EP EP12187065.3A patent/EP2586710A1/en not_active Withdrawn
- 2012-10-26 CN CN2012104145142A patent/CN103085966A/en active Pending
- 2012-10-26 US US13/661,454 patent/US9017511B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20130108828A1 (en) | 2013-05-02 |
US9017511B2 (en) | 2015-04-28 |
CN103085966A (en) | 2013-05-08 |
EP2586710A1 (en) | 2013-05-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |